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    CHAPTER 2

    TORSION IN RC BEAMS

    Prepared By Mesfin D.

    1

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    Torsion when encountered in reinforced concrete members

    usually occurs in combination with flexure and transverseshear. Due to this Torsion in its pure form (generally

    associated with metal shafts) is rarely encountered in

    reinforced concrete.

    Equi libr ium tors ion and compatib i li ty tors ion This is associated with twisting moments that are developed

    in a structural member to maintain static equilibrium with the

    external loads.

    are independent of the torsional stiffness of the member. Such torsion must be necessarily considered in design.

    INTRODUCTION

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    3

    Such type of torsion is induced in beams supporting lateral

    overhanging projections, in beams curved in plansubjected to gravity loads, and in beams where the

    transverse loads are eccentric with respect to the shear

    centre of the cross-section.

    fig.1a). Example of

    Equilibrium torision

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    This is the name given to the type of torsion induced in a

    structural member by rotations (twists) applied at one ormore points along the length of the member.

    The twisting moments induced are directly dependent on

    the torsional stiffness of the member.

    These moments are generally statically indeterminate.

    Their analysis necessarily involves (rotational)

    compatibility conditions; hence the name compatibility

    torsion.

    Torsions due to compatibility torsion are not necessaryfor equilibrium and may be neglected in ultimate limit

    state calculations and Design.

    Compatib i li ty Tors ion

    4

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    Members subjected to a torsional moment develop shear

    stresses.

    In general, these tend to increase in magnitude from the

    longitudinal axis of the member to its surface.

    If the shear stresses are sufficiently large, cracks will

    propagate through the member and, if torsion

    reinforcement is not provided, the member will collapsesuddenly.

    circu lar member sub jected to a torque T

    Torsional s tresses

    6

    a). Circular member b). Member in Torsion c . Shear distribution

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    shear stress at a given cross-section varies linearly from the

    longitudinal axis of the member to a maximum value, max, atthe periphery of the section.

    The stress at any distance r from the longitudinal axis of a

    circular member is given by:

    The maximum shear stress, maxis found by setting r= /2 in

    equation (1).

    7

    34max

    16

    32/

    2

    TT

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    But for non-circular member, the distribution of shearstress is not straightforward.

    rectangular member sub jected to a torque T

    Contd

    8

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    Contd

    9

    Unlike in the circular member, the stress distribution in arectangular member is non-linear.

    The maximum shear stress occurs at the mid-point of the

    longer side.

    Shear stress at the corners of the section is zero indicatingthat the corners of the section are not distorted under torsion.

    Analytical studies have shown that the maximum shear stress,

    max, in rectangular section is given by:

    The parameter depends on the relative values of x and y.

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    The stress distribution in thin-walled hollow members is

    much easier to determine than for solid non-circularmembers.

    The shear stress in the walls is reasonably constant and is

    given by:

    Thin-wal led ho l low member sub jected to a

    torque T

    10

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    Where t is the thickness of the wall of the member and

    Aois the area within a perimeter bounded by the centreline of the wall.

    On a given section, the shear stress is maximum where

    the thickness of the wall is minimum.

    Fai lure of conc rete members w i th tors ion Consider a rectangular member subjected to a torque T

    11

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    Consider small elements on each face of the member, as

    illustrated in the figure.As for members with applied shear, shear stresses act on

    the sides of each element in the directions.

    The equivalent principal stresses are inclined at an angle

    of 450to the horizontal. In the same way as for shear, the principal tensile stresses

    cause the development of cracks inclined at an angle of

    450.

    However, in the case of torsion, they form a spiral crack allaround the member

    Since the shear stresses in members with torsion are

    greatest at the surface, these cracks develop inwards from

    the surface of the member.

    (Contd...)

    12

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    For members with no form of reinforcement to preventthe opening of Torsional cracks, failure of the member

    will occur almost as soon as the cracking begins.

    Therefore, torsional failure of a member without

    reinforcement is prevented only if the shear strength of

    the concrete exceeds the shear stress due to applied

    torsion.

    The torsional strength of a concrete member can be

    significantly increased by providing suitable torsion

    reinforcement across the cracks.

    This is usually provided in the form of closedfour-sided

    stirrups, in combination with longitudinal bars distributed

    around the periphery of the section.

    (Contd...)

    13

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    This reinforcement controls the propagation of cracks and

    ensures that when failure occurs due to yielding of the

    reinforcement, it is not sudden. To quantify the behavior of members with such torsional

    reinforcement, an equivalent space truss model, similar to

    the plane truss model for shear, can be used.

    (Contd...)

    14

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    This theory, developed by Lampert and Collins(1972),

    assumes that solid members can be designed as equivalentthin walled hollow members .

    The thickness of the wall, t, is commonly taken as:

    15

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    The concrete cracks are inclined at an angle which,

    like shear, varies in the range 220< < 680.

    The truss dimensions,xoand yo, are measured from

    centre to centre of the notional thin walls.

    (Contd...)

    16

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    Since the horizontal projection of the crack is yo(cot ),

    the number of stirrups crossing the crack is yo(cot )/swhere sis the stirrup spacing.

    Hence, assuming that reinforcement has yielded, the

    total vertical shear force transmitted across the cracks by

    the stirrups on one side face is:

    Similarly the shear force transferred across the top or

    bottom face is:

    (Contd...)

    17

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    The shear force on the side wall of a thin walled member is

    Substituting for from equation (3) to equation (7) gives:

    Similarly it can be shown that:

    (Contd...)

    18

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    Substituting from equation (5) into equation (9)

    Thus the stirrup reinforcement required to resist torsion

    of Tis:

    In addition to the stirrup reinforcement, longitudinal

    reinforcement is required to resist torsion.

    (Contd...)

    19

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    From equilibrium of forces, the compressive force in the

    diagonal members, C, must equal V1/sin.

    And the force in the longitudinal members is

    N = Ccos = V1cot.

    20

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    Substituting for V1

    The total force in the longitudinal members from all four

    joints at a given cross section is:

    21

    cot2cot2cot2 2121 VVVVNTotal

    cot2 21 VVf

    ANTotals

    y

    long

    cotcot22

    200

    00

    00 yx

    yxTy

    T

    x

    TfAs

    y

    long

    cot

    00

    00

    sy

    long

    fyx

    yxTA

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    Alternatively, it can be rearranged to give the maximum

    torsion carried without leading to yielding of thelongitudinal reinforcement:

    Regardless of how much stirrup and longitudinal

    reinforcement is provided, the torsion must not be of

    such magnitude as to cause crushing of the concrete in

    the diagonal struts.

    This force is resisted by stresses in the concrete

    between the diagonal cracks.

    22

    cot00

    00

    yx

    fyxAT

    sy

    long

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    23

    The surface area of concrete to which this is applied is,

    from Fig. yo(cos ) t, Hence the stress in the struts is:

    This must not exceed the compressive strength of

    concrete, fck/c, where is the effectiveness factor for

    torsion

    cossincos

    sin

    0

    1

    0

    1

    ty

    V

    ty

    V

    strutinstress

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    Substitution for V1 from equation (7) gives:

    From which the torsion which could cause crushing of

    the concrete struts is Tw, is:

    24

    cckf

    tyV

    cossin0

    1

    cckf

    tyxT

    cossin2

    0

    0

    c

    ck

    w

    ftyxT

    cossin200

    Members with combined actions

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    For members with combined M and T, the longitudinal

    reinforcement required for torsion should be provided in

    addition to the amount required for moment.

    For members with combined T and V, the ultimate

    torque, T, and the ultimate shear force, V, should satisfy

    the condition:

    Members with combined actions

    25

    1

    22

    ww VV

    TT

    Design o f members for tors ion

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    26

    Design o f members for tors ion

    in acco rdance w ith EBCS2

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    The torsional resistance of members is calculated

    on the basis of an equivalent thin-walled section (i.e.the truss analogy) as describe above.

    Wall thickness t=teff=hef A/u the actual wall

    thickness

    For sections of complex shape, such as T-sections,

    the torsional resistance can be calculated by

    dividing the section into individual elements of

    simple, say rectangular, shape.

    The torsional resistance of the section is equal to

    the sum of the capacities of the individual elements,

    each modeled as an equivalent thin-walled section.

    Contd.

    27

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    The critical section for torsion is at the face of supports.

    Tsd does not exceed the torsional capacity, TRd whereTRd= 0.80fcdAefhef Aef= xoyo

    The torsional resistance of concrete Tcshall be taken as:

    The torsional resistance of the reinforcement Teffis given

    by:

    Members with pure torsion

    28

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    350mmor8

    S

    effU

    Spacing

    29

    yk

    wf

    4.0min,

    Members w i th combined

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    Members subjected to combined moment and tors ion

    The longitudinal reinforcement required for torsion andFlexure should be calculated separately and hence total

    area of reinforcement to be provided should be the sum

    of the two.

    Members sub jected to combined shear and to rs ion

    TRd and VRd(TRd= 0.80fcdAefhef and VRd= 0.25fcdbwd),

    respectively, multiplied by the following reduction factors

    tand v.

    Members w i th combined

    act ions

    30

    2

    1

    1

    RdSd

    RdSd

    t

    TT

    VV

    2

    1

    1

    RdSd

    RdSd

    v

    VV

    TT

    RdVvRdVRdTtRdT 'and'

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    Tcand Vc(Tc= 1.2fctdAefhef and Vc= 0.25fctdk1k2bwd),

    respectively, must be multiplied by the reduction factorstcand vc.

    The calculations for the design of stirrups may be made

    separately for torsion and shear and the total stirrup

    required for shear and torsion are, of course, additive.

    31

    2

    1

    1

    cSd

    cSd

    tc

    TT

    VV

    2

    1

    1

    cSd

    cSd

    vc

    VV

    TT

    cVvcVTtcT ccc 'and'

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    .

    .

    .

    32

    S

    A

    S

    A

    S

    Atvtv

    2

    torsionandshearforstirrupleg2Total

    ydeff

    effst

    fA

    T

    S

    A

    *2

    )(

    leg1 torsionforStirrup

    df

    V

    S

    A

    yd

    sdv

    *

    hear2 SforStirrupleg

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    33

    THE END